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This section includes 454 Mcqs, each offering curated multiple-choice questions to sharpen your Mechanical Engineering knowledge and support exam preparation. Choose a topic below to get started.
451. |
High air-fuel ratio in gas turbines |
A. | Increases power output |
B. | Improves thermal efficiency |
C. | Reduces exhaust temperature |
D. | Do not damage turbine blades |
Answer» D. Do not damage turbine blades | |
452. |
Adiabatic compression is one in which |
A. | Temperature during compression remains constant |
B. | No heat leaves or enters the compressor cylinder during compression |
C. | Temperature rise follows a linear relationship |
D. | Work done is maximum |
Answer» C. Temperature rise follows a linear relationship | |
453. |
In multistage compressor, the isothermal compression is achieved by |
A. | Employing inter-cooler |
B. | By constantly cooling the cylinder |
C. | By running compressor at very slow speed |
D. | By insulating the cylinder |
Answer» D. By insulating the cylinder | |
454. |
A simple turbojet engine is basically |
A. | A propeller system |
B. | Gas turbine engine equipped with a propulsive nozzle and diffuse |
C. | Chemical rocket engine |
D. | Ramjet engine |
Answer» C. Chemical rocket engine | |